New type aircraft

ABSTRACT

The present invention relates to a new type aircraft. The aircraft includes the airframe and wing, characterized in that the transverse section of airframe has an oblate (oval) profile with corrugated area on the ventral of airframe; the aircraft has uneven friction areas on the underside surface of wing; there are fireproof &amp; anti-wear layers on the envelopes of airframe ventral and friction areas; the said fireproof &amp; anti-wear layers have tire rubber material. When the aircraft is in motion with high velocity, the friction with air is increased, which produces bigger lift with more aircraft load and shortened takeoff &amp; landing distance of aircraft, meanwhile the safe peril to aircraft caused by the shear transformation of wind in flight is prevented effectively; the fireproof &amp; anti-wear layers on the envelopes of airframe ventral and friction areas have an effect on higher anti-wear proof and longer aircraft life.

FIELD OF THE INVENTION

[0001] The present invention relates to an aircraft, especially relatesto an unique structural new type aircraft.

BACKGROUND OF THE INVENTION

[0002] It has been over 100 years since the “Reiter” brother in U.Sinvented an aircraft whose theory of aircraft lift was based on the wingstructure of circular on top & flat on bottom. With this wing structureof circular on top & flat on bottom, the resistance was decomposed to adownward “ballast force” in aircraft high velocity flight, so the safetyand reliability in high velocity flight was ensured. The ballast forceis proportional to the flight velocity and the aircraft could keep thesmooth & effective controlling even in high velocity flight. Theaircraft, However, may loop the loop and even flight turn over in sky,in this way, the wing structure of circular on top & flat on bottomproduced no so called “lift force” but a downward “ballast force” withwhich the high velocity flight of aircraft was ensured in practice. Andthis point may be clear from the flight orbit of aircraft. In view ofthis, the invention put forwards a new lift theory absolutely differentfrom one of “Reiter” brother's.

BRIEF DESCRIPTIONS OF THE INVENTION

[0003] This invention is based on repudiating the lift theory raised bythe “Reiter” brother in U.S and establishing a absolutely new “actingforce & reacting force” lift theory, and supplies a new type aircraftwhose lift force is increased in flight with benefits of more load,shortened takeoff & landing distance and decreased safe peril toaircraft caused by the shear transformation of wind in flight.

[0004] The purpose of this invention is realized through the followingtechnologies.

[0005] The new type aircraft includes the airframe and wing,characterized in that the transverse section of airframe has an oblate(oval) profile with corrugated area on the ventral of airframe.

[0006] Said new type aircraft has uneven friction areas on the undersidesurface of wing; There are fireproof & anti-wear layers on the envelopesof airframe ventral and friction areas.

[0007] In said new type aircraft, the said fireproof & anti-wear layershave tire rubber material.

[0008] In the new type aircraft supplied by the present invention, owingto the airframe has an oblate (oval) profile with corrugated area on theventral of airframe, when the aircraft is in motion with high velocity,the friction area with air is increased, which produces bigger lift withmore aircraft load and shortened takeoff & landing distance, meanwhilethe safe peril to aircraft caused by the shear transformation of wind inflight is prevented effectively; the fireproof & anti-wear layers on theenvelopes of airframe ventral and friction areas have an effect onhigher anti-wear and longer aircraft life.

BRIEF DESCRIPTION OF THE APPENDED DRAWINGS

[0009]FIG. 1 is a structural illustrative view showing the new typeaircraft in embodiment 1.

[0010]FIG. 2 is a transverse section illustrative view of FIG. 1.

DESCRIPTION OF FIGURE MARKS

[0011]1: airframe, 1-1: corrugated area, 2: wing, 2-1: friction area, 3:fireproof & anti-wear layer.

DETAILED DESCRIPTION OF THE INVENTION

[0012] Next, a further description will be made as to the new typeaircraft provided by present invention with the Specification Figures:

[0013] Embodiment: Manufacturing the aircraft profile as FIG. 1 withcorrugated area 1-1 on ventral of airframe 1, making airframe 1 to anoblate (oval) profile as FIG. 2. There are uneven friction areas 2-1 onthe underside surface of wing 2 and the friction areas 2-1 are forincreasing the friction factor in flight, there are fireproof &anti-wear layers 3 of 0.2-0.3 cm thick on the envelopes of ventral ofairframe 1 and friction areas 2, and the fireproof & anti-wear layershave tire rubber material of high carbon contents. The aircraft producesbig friction with air in high velocity flight; for the huge weight ofaircraft and based on the “acting force & reacting force” relationshipin the Newton Mechanics, the reacting force rubbing with air under wing2 and ventral is acting onto the airframe 1 as FIG. 2 shows and the liftis increased to realize this invention purpose.

We claim:
 1. A new type aircraft, includes airframe (1), wing (2),characterized in that the transverse section of airframe (1) has anoblate (oval) profile with corrugated area (1-1) on the ventral ofairframe (1).
 2. A new type aircraft according to claim 1, characterizedin that there are uneven friction areas (2-1) on the underside surfaceof wing (2).
 3. A new type aircraft according to claim 1, characterizedin that there are fireproof & anti-wear layers (3) on the ventralenvelopes of airframe (1).
 4. A new type aircraft according to claim 2,characterized in that there are fireproof & anti-wear layers (3) on thefriction areas (2-1).
 5. A new type aircraft according to claim 3,characterized in that the said fireproof & anti-wear layers (3) havetire rubber material.
 6. A new type aircraft according to claim 4,characterized in that the said fireproof & anti-wear layers (3) havetire rubber material.